Multi-beam heterodyne laser doppler vibrometer

ABSTRACT

A multi-beam heterodyne vibrometer for analyzing vibration of an object includes an optical system and a combining element. The optical system generates a plurality of object beams and a plurality of reference beams where one of the plurality of beams has a frequency that is shifted from a frequency of the other plurality of beams. The optical system focuses each of the plurality of object beams on the object and transmits the plurality of focused object beams to the object. A portion of each of the plurality of focused object beams is reflected off of a surface of the object as a modulated object beam. The optical system collects the modulated object beams. The combining element combines each of the modulated object beams with a respective one of the reference beams into a plurality of beam pairs.

CROSS REFERENCE TO RELATED APPLICATIONS

The present application is a continuation-in-part application of U.S. patent application Ser. No. 11/262,707 filed Oct. 31, 2005 now U.S. Pat. No. 7,116,426, which is a continuation of U.S. patent application Ser. No. 10/405,045 filed Mar. 31, 2003, and now issued as U.S. Pat. No. 6,972,846.

STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH

This invention was made with government support under Contact Numbers DAAB07-00-C-F602 and DAAB07-01-C-L853 awarded by the United States Department of Defense to MetroLaser, Inc. The government has certain rights in the invention.

BACKGROUND OF THE INVENTION

1. Technical Field

The present invention is related to the measurement of vibration using non-invasive, non-contact, and remote techniques; namely, multiple beams of coherent radiation are used as a probe to simultaneously measure vibrations at multiple locations on an object.

2. Description of the Related Art

Laser Doppler Vibrometry (LDV) is a well-known non-contact method to measure the vibration of an object. Fields of application include: automotive, aerospace, and civil engineering; landmine detection; non-destructive testing; and non-contact sensing. LDV techniques are based on the use of an interferometer to measure the Doppler frequency shift of light scattered by a moving object. The motion of the object relative to the light source causes a shift of the light's frequency as described by the Doppler equations.

There are two interferometric methods conventionally used for LDV applications: homodyne detection and heterodyne detection. An optical quadrature homodyne interferometer is a simple design utilizing low-frequency photodetectors and amplifiers. However, the non-linear behavior of these components causes harmonic distortions of the measured signal and an overall reduction in accuracy.

The heterodyne detection method using frequency shifting techniques overcomes a number of drawbacks inherent in homodyne detection, including: (a) harmonic doubling that occurs when a source is located a multiple number of wavelengths away from the target or object under analysis; (b) non-linearity that occurs at vibration amplitudes on the order of the measurement radiation's wavelength; (c) a low signal-to-noise ratio caused by sensitivity to laser intensity fluctuations; and (d) inverse frequency (i.e., 1/f) detector noise. Both homodyne and heterodyne LDV systems based on single-point measurement techniques have been extensively investigated and form the basis of various conventional commercial instruments.

Devices consisting of a single-beam LDV system in concert with a beam scanning system have also been developed. Scanned single-beam techniques are suitable for measuring vibrations that are repetitive (e.g., continuously cycling over the same location); however, because the measurements are made sequentially from one location to the next, the value of this technique is limited when the vibrations are transient or non-repetitive. Measurement of non-repetitive vibrations is important when analyzing civil structures, aerospace composite components, and golf clubs, as well as for buried land mine detection. While a plurality of single-beam LDV systems could be used to measure multiple locations on an object, this would be a costly and complicated option if a large number of simultaneous measurements were required.

Simultaneous measurement of multiple locations on an object is needed in order to gain more complete data on an object's vibrational characteristics. Specifically, simultaneous LDV measurements yield: (a) phase information among the measured points, (b) increased inspection speed, and (c) the ability to measure non-repetitive vibration patterns. A simultaneous multi-beam LDV system based on a homodyne interferometer design has also been investigated. However, because that multi-beam technique is based on a homodyne detection method, it is affected by the same performance limitations as the single-beam homodyne system described above.

In view of the foregoing, there is a need in the art for an LDV device that can simultaneously measure multiple locations on an object with the benefits of high signal-to-noise ratio, wide dynamic range, and high accuracy inherent with heterodyne detection.

BRIEF SUMMARY OF THE INVENTION

A heterodyne Multiple-Beam Laser Doppler Vibrometer (MBLDV) simultaneously measures displacement or velocity history of a multitude of locations on an object or multiple objects. Simultaneous heterodyne measurement of multiple locations provides a highly accurate measurement of an object's vibrational characteristics, especially transient vibrations. Such precise measurement of non-repetitive vibrations enhances the capability of laser Doppler velocimetry.

According to one aspect of the invention, a multi-beam heterodyne vibrometer includes an optical system and a combining element. The optical system generates a plurality of object beams and a plurality of reference beams where one of the plurality of beams has a frequency that is shifted from a frequency of the other plurality of beams. The optical system focuses each of the plurality of object beams on the object and transmits the plurality of focused object beams to the object. A portion of each of the plurality of focused object beams is reflected off of a surface of the object as a modulated object beam. The optical system collects the modulated object beams. The combining element combines each of the modulated object beams with a respective one of the reference beams into a plurality of beam pairs. The beam pairs may then be detected to provide a detection signal, the detection signal being processed to determine one or more characteristics of the object.

One of the advantages of the invention is that the vibrometer is able to simultaneous measure velocity or displacement of an object over multiple points. The heterodyne technique utilized by the vibrometer enables measurements near zero frequency or velocity with excellent fidelity. Measurements made by the vibrometer of the invention are characterized by high signal-to-noise ratio, wide dynamic range, and simple alignment. The system may utilize a computer with software for computing and displaying the velocity and/or amplitude history of all of the measured points of the object.

Other features and advantages of the present invention will become apparent to those skilled in the art from a consideration of the following detailed description taken in conjunction with the accompanying drawings. The terms invention and embodiment as described herein refer to one or more embodiments of the present invention.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a block diagram of a multi-beam laser Doppler vibrometer (MBLDV) system of the invention;

FIG. 2 is a schematic view of a MBLDV implemented in an object-detection embodiment;

FIG. 3 is a flow chart illustrating a methodology according to a number of embodiments of the invention;

FIG. 4 is a schematic view of a MBLDV according to some of the embodiments;

FIG. 5 is a schematic view of an embodiment of an analyzing portion of the MBLDV system;

FIG. 6 is a schematic view of another embodiment of the analyzing portion;

FIG. 7 is a block diagram that schematically illustrates general principles of the invention;

FIGS. 8A and 8B schematically illustrate beam-splitting principles of the invention according to a number of embodiments;

FIGS. 9A and 9B schematically illustrate beam-splitting principles of the invention according to other embodiments;

FIGS. 10A and 10B schematically illustrate principles for directing a beam onto a beam splitter according to still other embodiments;

FIG. 11 is a schematic view of an embodiment of a collecting and combining portion of the invention;

FIG. 12 is a schematic view of another embodiment of the collecting and combining portion of the invention;

FIG. 13 illustrates an optical relationship between a focusing lens and an output element of the invention; and

FIG. 14 is a schematic view of a MBLDV implemented in a scanning embodiment.

FIG. 15 is a schematic view of a MBLDV optical subsystem according to an embodiment having an objective lens assembly.

Embodiments of the present invention and their advantages are best understood by referring to the detailed description that follows. It should be appreciated that like reference numerals are used to identify like elements illustrated in one or more of the figures. A more complete understanding of embodiments of the present invention will be afforded to those skilled in the art, as well as a realization of additional advantages thereof, by a consideration of the following detailed description.

DETAILED DESCRIPTION

A multiple-beam laser Doppler vibrometer (MBLDV) of the invention simultaneously measures the vibrational characteristics at multiple locations on a target or object. The MBLDV may be utilized in a number of different applications. For example, in a number of embodiments the MBLDV may be used in concert with acoustic techniques to measure transient vibrations in a land mine detection system. In other embodiments the MBLDV may be used to find internal flaws in structural components (e.g., composite materials, honeycomb, etc.). The MBLDV may also be used with or without additional acoustic excitation to measure vibration on automotive components, vibration on aircraft components, vibration on musical instruments, vibration on office machines (e.g., copiers and computers). In other embodiments the MBLDV may be used to measure vibration from bridges and civil engineering structures.

Referring to the drawings in more detail, a block diagram of an exemplary embodiment of a MBLDV system 9 is illustrated in FIG. 1. Multiple beams T (shown in solid line) are transmitted to and illuminate an object 10 under inspection, and back-scattered radiation M (shown in dashed line) from the beams T is collected by an optical sub-system 11 (or subsystem 11). In a number of embodiments, the optical system processes the back-scattered radiation M and provides data associated with the radiation M to an electronics subsystem 12.

Depending upon the application, the electronics subsystem 12 may further process the data prior to providing the data to an analysis subsystem 13. After analysis, the data may be provided to a data output subsystem 14. In some of the embodiments, subsystems 11, 12, 13, and 14 may be incorporated as a single-unit MBLDV 15. The data output subsystem 14 of the MBLDV 15 may provide processed data to a data collection and display system 16 of the system 9.

According to a number of embodiments, the MBLDV system 9 may be configured as a buried land mine detection system, which is depicted in FIG. 2. In these embodiments, the system 9 may include the MBLDV 15 and an audio source 17 such as a speaker. Acoustic vibrations V from the audio source 17 send vibrations into the ground G. When coupled to a buried object 10 a, vibrations B modulate the surface S of the soil. The transient vibrations of the soil may then be measured by the MBLDV 15 to detect the object 10 a. In this embodiment, the transmitted object beams Ts are scattered and/or reflected by the soil S, not the object 10 a necessarily.

The system 9 illustrated in FIG. 2 may also be utilized in a nondestructive testing embodiment. In these embodiments, the object 10 a may be a subsurface flaw, which flaw is detected by the MBLDV 15 after excitation from an acoustic source 17. In other embodiments, the MBLDV 15 may analyze self-excitation objects such as loud speakers and engines.

Referring to FIG. 3, in a number of embodiments the MBLDV system 9 operationally may provide a coherent laser source 18 which is divided into an object beam and a reference beam at process 19. At process 20 the object beam may be divided into a plurality of object beams, which, at process 21, may then be focused onto a targeted object 10. Vibrations at multiple locations on the object 10 modulate the multiple object beams simultaneously. The modulated object beam radiation is scattered and/or reflected back by the object 10, which is also know as backscattering. At process 22, this reflected and scattered radiation from the object 10 may be collected by the optical subsystem 11 of the MBLDV 15.

Regarding the reference beam, at process 23 a frequency shift may be added to the reference beam. In a number of embodiments, the frequency-shifted reference beam may be referred to as a local oscillator. At process 24 the frequency-shifted reference beam may be divided into a plurality of reference beams. At process 25 the modulated reflected and scattered radiation from the object and the plurality of frequency-shifted reference beams may be combined and, at process 26, focused into a plurality of fiber optics or detectors.

At process 27 data collected by the detectors may be analyzed. For example, surface displacement of each of the object beams may be calculated using a computer, displayed on a monitor, or output to a peripheral device of the display and collection system 16.

In alternative embodiments, rather than utilizing a frequency-shifted reference beam, the MBLDV 15 may be configured to frequency shift the object beam. The resulting frequency-shifted object beam may be split into a plurality of frequency-shifted object beams that are transmitted to the object. In this regard, the optical beam path in FIG. 3 may include process 23 in which a frequency shift is added to the object beam prior to process 20 in which the beam is divided.

With reference to FIG. 4, according to a number of embodiments, the optical sub-system 11 may include a laser 18 as a radiation source. For example, the laser 18 may be a single continuous-wave frequency-stabilized diode-pumped Nd:YAG laser that produces an ultra-narrow line-width 532 nm beam with a single axial mode.

The output beam L of the laser 18 is reflected by a mirror 28 a. A first half-waveplate (HWP) 29 may be positioned downstream of the mirror 28 a to rotate the polarization of the beam and thus provide variable control of the irradiance of beams downstream thereof. The output beam L may then be split into an object beam O and a reference beam R at a first polarizing beam splitter (PBS) 30. As shown in the example in FIG. 4, the S-polarized portion of the output beam L is reflected by the PBS 30 and used as the object beam O, and the P-polarized portion of the output beam L is transmitted by the PBS 30 and used as the reference beam R. (For purposes of this description, the conventional scientific notation for polarization is used in the drawings, i.e., an arrow for P-polarization and a dot for S-polarization.)

Regarding a path of the object beam O (i.e., the object path), a second HWP 31 may be positioned downstream of the PBS 30 to rotate the object beam O to P-polarization. A telescope formed by a first lens 32 and a second lens 33 may be utilized to expand the object beam O from where the object beam O is incident at a first (or object) diffractive optical element (DOE) 34, which splits the object beam O into a plurality of object beams Os. The lenses 32 and 33 may also focus the object beams Os onto the targeted object 10. The plurality of object beams Os may then be transmitted through a second PBS 35 and a quarter-waveplate (QWP) 36 and then transmitted to the object 10 under inspection, which transmitted object beams are indicated by Ts. The plurality of transmitted object beams Ts irradiate substantially and simultaneously a corresponding plurality of points on the object 10.

In alternative embodiments, a plurality of lasers, beam splitters, and other optical element may be used to split an object beam into a plurality of object beams. Furthermore, the pattern of the object beams may follow different geometries depending on the choice of beam splitter. For example, in the embodiment shown in FIG. 4, the object beam O is linearly split into a plurality of object beams Os. In other embodiments, the object beam O may be split into a plurality of object beams that form a matrix of X columns and Y rows. In still other embodiments, the optical subsystem 11 may include arbitrary multiple beam patterns and scanning of the beams.

Vibrations of the object 10 frequency modulate each of the transmitted object beams T substantially simultaneously. A portion of these modulated object beams, which are indicated by Ms, is scattered and reflected back to the optical subsystem 11. In the embodiment shown in FIG. 4, the modulated object beams Ms may pass through the QWP 36 and rotate to S-polarization. The modulated object beams Ms may then be reflected at the PBS 35 and collected by a lens 37. Downstream of lens 37 may be positioned a beam combiner 38 or combining element, a lens 39, an optical output 40, and a sensing element 41, which will be discussed in more detail below. Beam combiner 38 may be a non-polarizing beam splitter (BS), a polarizing beam splitter (PBS), a beam splitter cube, or a beam splitter plate that may be used to split or combine light beams. Further, the optical components discussed herein may optionally include an optical coating such as an anti-reflective (AR) coating.

Turning to a path of the reference beam R (i.e., the reference path), in the embodiment shown in FIG. 4 the reference beam R may be initially frequency shifted. To do so, in a number of embodiments the reference beam R may travel sequentially through one or more acousto-optic modulators. In the embodiment shown, two acousto-optic modulators (AOM) 42 and 43 are employed. In some of the embodiments, the AOMs 42 and 43 may be operated at different frequencies, for example, frequency f₁ and frequency f₂, respectively, so that different diffraction orders of the reference beam R may be selected. For example, the first AOM 42 operating at frequency f₁ may select the +1^(st) order diffracted beam of the reference beam R, and the second AOM 43 operating at frequency f₂ may select the −1^(st) order diffracted beam of the reference beam R. In this example, the reference beam R is frequency shifted by the difference of frequencies f₁ and f₂. As an example, AOM 42 operating at a frequency of 80 MHz and AOM 43 operating at a frequency of 80.1 MHz produce a frequency shift of 100 kHz on the reference beam R.

In other embodiments of the invention, the object beam O can be frequency shifted to achieve a carrier frequency that yields a typical heterodyne signal in detectors of a detector array. As in the case of the reference beam, this frequency shift may be obtained with a single AOM, two AOMs, or various other devices such as rotating gratings, micro-electromechanical system (MEMS), liquid crystal gratings, and other devices to shift the frequency of the beams.

Upon being frequency shifted, the reference beam R may be reflected by a mirror 28 b through a third HWP 44 to rotate the reference beam R to S-polarization so that the reference beam R has the same polarization as the collected modulated object beams Ms after they pass through the quarter waveplate 36 and beamplitter 35. The reference beam R may then be expanded and collimated by a telescope formed by a first lens 45 and a second lens 46.

The collimated reference beam R may then be reflected from a mirror 28 c through a second (or reference) DOE 47. In a number of embodiments, the reference DOE 47 may be identical to the object DOE 34. The reference DOE 47 splits the reference beam R into a plurality of reference beams. In embodiments in which the DOES 34 and 47 are substantially the same, the number of object beams is equal to the number of reference beams (e.g., 16); in addition, the angle at which the object beams diverge from the object DOE 34 is substantially equal to the angle at which the reference beams diverge from the reference DOE 47. For example, the DOEs 34 and 47 may split the beams O and R into 16 beams Os and Rs, respectively, which beams diverge from the DOEs at an angle of about 22 degrees. Those skilled in the art will appreciate that the DOEs 34 and 47 may be modified to produce any number of beams that diverge at any angle.

Upon splitting, the reference beams Rs may be reflected from a mirror 28 d toward the beam combiner 38. In accordance with a number of embodiments, the beam combiner 38 combines each of the plurality of reference beams Rs with a respective one of the modulated object beams Ms, thereby yielding a corresponding plurality of beam pairs Ps, wherein each beam pair P includes a modulated object beam M and a frequency-shifted reference beam R. In some of the embodiments, the beam combiner 38 aligns each of the reference beams Rs to overlap with one of the modulated object beams Ms.

The plurality of beam pairs Ps may then be focused on an optical output, such as a plurality of optical fibers 40, which may be coupled to a detecting element, such as a plurality of photodetectors 41 located in the electronics subsystem 12 configured to detect the plurality of beam pairs to produce a plurality of beam pair signals. The plurality of beam pair signals may be processed to determine one or more characteristics of the object under analysis. Lenses 37 and 39 focus or image the modulated object beams Ms onto the optical fibers 40. In other embodiments the plurality of photodetectors may replace the optical output so that the beam pairs Ps focus directly on the photodetectors. In other embodiments the detecting element may include coherent fiber-optic cable/bundles, photodiodes, CMOS detector arrays, or CCD detector arrays.

Each of the detectors 41 senses a frequency-modulated signal of a beam pair P. The frequency-modulated signal of each beam pair P has a carrier frequency f_(c) given by the difference of the frequencies of the AOMs 42 and 43, namely, f_(c)=f₁−f₂. In addition, frequency-modulated signal of each beam pair P has a frequency deviation caused by vibration of the object 10.

In a number of embodiments, in addition to providing an interface for the signals output by the optical subsystem 11, the electronics subsystem 12 may provide power to and filtering functions for the detectors 41. Further, the electronics subsystem 12 may be coupled to the AOM 42 and 43 to provide power and drive signals to the AOMs for frequency shifting the reference beam R.

As mentioned, each optical fiber 40 of the optical subsystem 11 may be coupled to a photodetector 41 of the electronic subsystem 12. Each of the detectors 41 has a bandwidth that may be chosen to be larger than the carrier frequency f_(c) of the beam pairs Ps. For example, if frequency f₁ of AOM 42 is 80.0 MHz and frequency f₂ of AOM 43 is 80.1 MHz, then the bandwidth of the detectors 41 may be larger than 100 kHz (i.e., f₁−f₂), for example, about 1 MHz.

Referring to FIG. 5, in a number of embodiments, the electronics subsystem 12 may include a reference clock 48 for generating the carrier frequency f_(c). In some of the embodiments, the clock 48 may include a pair of radio frequency (RF) drivers 49 and 50 respectively operating at frequency f₁ and frequency f₂, which frequencies may be provided to the AOMs 42 and 43, respectively. An electronic mixer 51 may mix frequencies f₁ and f₂ to generate a frequency equal to the sum (f₁+f₂) and a frequency equal to the difference (f₁−f₂). A low-pass filter 52 may be positioned downstream of the mixer 51 to eliminate the sum frequency, thereby providing a carrier signal C at the frequency f_(c).

The electronics subsystem 12 may also include a pair of bandpass filters 53 and 54 each of which is centered at the carrier frequency f_(c) (i.e., f₁−f₂). The filters 53 and 54 maintain a high signal-to-noise ratio in frequency-modulated signals Fs output from the detectors 41 and the carrier signal C output from the reference clock 48. In those embodiments in which a plurality of optical fibers 40 respectively receive the plurality of beam pairs Ps (see FIG. 4), each of the frequency-modulated signals Fs corresponds to a respective one of the beam pairs Ps and, accordingly, to a respective one of the modulate object beams Ms.

The carrier signal C from the reference clock 48 and the frequency-modulated signals Fs from the detectors 41 may then be digitized by a simultaneous sampling analog-to-digital (A-D) data-acquisition system 55. In a number of embodiments, the sampling rate of the A-D system 55 may be sufficiently large when compared to the carrier frequency f_(c); for example, if the carrier frequency f_(c) is about 100 kHz, then the sampling rate may be at least about 300 kHz.

When digitized, the frequency-modulate signals Fs and the carrier signal C may be provided to the analysis subsystem 13. In a number of embodiments, the analysis subsystem 13 utilizes software to analyze the signals Fs from the detectors 41. In a number of embodiments, the frequency-modulated signals Fs and the carrier signal C may be initially cleaned with one or more digital bandpass filters 56. The carrier signal C may then be phase-shifted 57, for example, by 90 degrees, with a software algorithm, such as a digital Hilbert transform.

The carrier signal C and the phase-shifted carrier signal may then be mixed with each of the frequency-modulated signals Fs, which is indicated at 58 and 59, respectively. Each of the mixed signals may then be low-pass filtered 60 and 61. The result of this digital processing are a set of in-phase signals I and a set of quadrature signals Q signals for each of the frequency-modulated signals Fs.

The in-phase and quadrature signals I and Q may then be processed by a processor 62 to determine a number of attributes of the object 10. For example, in a number of embodiments object displacement may be calculated utilizing the inverse tangent of the in-phase and quadrature signals I and Q. In addition, discontinuities at steps of 2π (i.e. 2pi) may be removed from signals I and Q by standard phase unwrapping techniques. Alternatively, object velocity may be calculated from the quantity: [(I′×Q)−(I×Q′)]÷[I ² +Q ²].

In a number of embodiments, when the displacement (or the velocity) of the object 10 has been calculated as a function of time for each of the frequency-modulated signals Fs, then signals I and Q may be Fourier analyzed to determine the displacement (or the velocity) as a function of frequency. The resulting Fourier spectra may then sent by a computer 63 of the display subsystem 16 to an output device, such as a monitor 64. Alternatively, the computer 63 may provide a hardcopy of the analyzed data to a printer 65 or transmit the data to a remote location 66, for example, over a network. A software package may be implemented on the computer 63 for processing data associated with the frequency-modulated signals Fs.

In a number of embodiments, the Fourier spectra may be displayed in a “waterfall”-type graph with a small offset applied to each spectrum so that all of the spectra can be viewed simultaneously. In addition, a one-dimensional or a two-dimensional surface map of the displacement (or the velocity) of the object 10 may be created at a given frequency band. To improve the processing speed of the analysis subsystem 13, displacement-versus-time signals can be safely down-sampled from the high sampling frequency (e.g., at least about 300 kHz) down to a low sampling frequency (e.g., less than 10 kHz), thereby resulting in faster Fourier transform calculations. Overall, each of the heterodyne signals Fs corresponding to each of the modulated object beams Ms may be simultaneously analyzed with one or more demodulation techniques.

Alternative embodiments of the electronics subsystem 12 and the analysis subsystem 13 are illustrated in FIG. 6. To maintain a high signal-to-noise ratio, the electronics subsystem 12 may include a pre-amplifier stage and an amplifier stage 67 to amplify the frequency-modulated signals Fs output from the detectors 41. In embodiments both analog and digital processing is desired, the frequency-modulated signals Fs may be provided to an analog output 68 through phase-locked loop (PLL) circuitry 69. Further, in addition to digitizing the frequency-modulated signals Fs and the carrier signal C with the A-D converter 55 for downstream conditioning by elements 56 to 61, the frequency-modulated signals Fs may be digitized by a second A-D converter 70, the output of which is fed directly to the processor 62.

With further reference to FIG. 2, according to a number of embodiments the vibrometer 15 may be configured to detect land mines. As mentioned above, a loudspeaker 17 may be utilized to generate acoustic waves V in the air, which couple into the ground G and cause the buried object 10 (i.e., a land mine) to vibrate. The vibrations of the object 10 (indicated by B) cause the soil S above the object 10 to vibrate. The MBLDV 15 may then be utilized to collect the modulated object beams Ms and analyze the resulting frequency-modulated signals Fs. For example, the velocity of the soil S at multiple points may be calculated. The presence of a buried object 10 can be determined by studying the spatial distribution of the soil velocity spectra.

Because of the plurality of transmitted object beams Ts, the MBLDV 15 is able to simultaneously measure a plurality of points, thereby substantially reducing the time required take the measurements necessary to detect a buried object 10. For example, if there are 16 transmitted object beams Ts, then the MBLDV 15 would reduce the necessary measurement time by a factor of 16 over conventional single-beam scanning systems. A one-dimensional beam array may then be translated in the cross-dimension, thereby providing coverage of a two-dimensional area in a much shorter time than a conventional scanning method.

According to a number of embodiments, the MBLDV 15 may be configured to detect both surface defects (e.g., cracks) and subsurface defects (e.g., disbonds, delaminations, etc.) in aircraft and ship panels. In these embodiments, the surface of a panel may be excited by an acoustic or mechanical source. The resulting surface displacement (or velocity) profile may then be examined with by the MBLDV system 9. The presence of a surface defect, such as a crack, causes a change in the vibrational pattern of the surface. The presence of a subsurface defect may cause an enhanced velocity above the defect at a particular resonance frequency. In contrast to conventional scanning devices where the surface must be excited repetitively, the MBLDV 15 of the invention is able to analyze a plurality of points simultaneously with a single excitation of the surface. In addition, the MBLDV 15 is able to provide the relative phase between each analyzed point so that modal vibrational patterns can be immediately observed.

In addition to detecting defects as described above, the MBLDV 15 has many other applications. For example, the vibration pattern of a test object may be measured, such as speakers, musical instruments, automotive disc brakes, computer disks, car panels, airplane panels, and so on. In these embodiments, the MBLDV 15 measures the vibration of the object without any additional acoustic excitation.

Turning to a more general description of the principles of the invention with reference to FIG. 7, a multi-beam heterodyne vibrometer 100 for analyzing vibration of an object 10 includes an optical system 102 and a combining element 104. In a number of embodiments, the optical system 102 generates a plurality of object beams T that are transmitted to the object 10 and a plurality of frequency-shifted reference beams R. The plurality of frequency-shifted reference beams R have a frequency that is shifted from a frequency of the plurality of transmitted object beams T. Alternatively, the optical system 102 generates a plurality of object beams T and a plurality of frequency-shifted reference beams R, where one of the plurality of one set of frequency-shifted reference beams has a frequency that is shifted from the frequency of the other plurality of object beams. A portion of each of the transmitted object beams T is scattered or reflected off of the object 10, thereby producing a plurality of modulated object beam M. The optical system 102 also collects the modulated object beams M reflected by the object 10. The combining element 104 combines each of the modulated object beams M with a respective one of the frequency-shifted reference beams R into a plurality of beam pairs P, which may be provided to a process stage 106.

Referencing FIGS. 8A and 8B, the optical system 102 includes a pair of beam splitters, such as the DOEs 34 and 47 (see FIG. 4), for respectively splitting the object beam O into the plurality of object beams Os and the frequency shifted reference beam R into the plurality of frequency-shifted reference beams Rs. DOE 34 is configured to split the object beam O so that the plurality of object beams Os diverge from an optical axis A of the DOE 34 at a divergence angle ω (i.e. omega). Similarly, DOE 47 is configured to split the frequency-shifted reference beam R so that the plurality of frequency-shifted reference beams Rs diverge from the optical axis A of DOE 47 at a divergence angle ρ (i.e. rho). The divergence of the object beams Os and the frequency-shifted reference beams Rs is also shown in FIGS. 9A and 9B. According to a number of embodiments, the DOEs 34 and 47 are configured so that divergence angle ω of the object beams Os is substantially the same as the divergence angle ρ of the frequency-shifted reference beams Rs.

With continued reference to FIGS. 9A and 9B, in other embodiments the DOEs 34 and 47 may be configured to split the object beam O and the frequency-shifted reference beam R, respectively, so that the number of object beams Os is equal to the number of frequency-shifted reference beams Rs. For example, the number of beams may be an exponential of 2, i.e., 2^(n) where n is an integer.

With additional reference to FIGS. 10A and 10B, the optical system 102 may also include a first telescope 108 for focusing or directing the object beam O onto one of the beam splitters, i.e., DOE 34, and a second telescope 110 for focusing or directing the frequency-shifted reference beam R onto the other one of the beam splitters, i.e., DOE 47. As shown in the drawings, in a number of embodiments, the first telescope 108 may include lenses 32 and 33 and the second telescope 110 may include lenses 45 and 46 of the embodiment illustrated in FIG. 4. As mentioned above, the first telescope 108 also focuses the plurality of object beams Os onto the object 10.

As shown in FIGS. 10A and 10B, the object beam O has a diameter d_(O), and the frequency-shifted reference beam R has a diameter d_(R). According to a number of embodiments, the telescopes 108 and 110 are configured to direct or closely collimate the object beam O and the frequency-shifted reference beam R, respectively, onto a respective one of the beam splitters, i.e., DOEs 34 and 47, respectively, such that the diameters of the beams O and R are substantially equal when incident upon the DOEs 34 and 47. The diameters of the object beam O and the frequency-shifted reference beam R when incident with the DOEs 34 and 47 are indicated by D_(O) and D_(R), respectively. For example, the first telescope 108 may slightly focus the object beam O onto DOE 34 so that a beam diameter D_(O) is produced at DOE 34, while sharply focusing the transmitted object beams Os at the target or object 10. The second telescope 110 may collimate the frequency-shifted reference beam R onto DOE 47 so that diameters D_(O) and D_(R) are substantially the same.

With reference to FIG. 11, the optical system 100 may include a collecting lens 37 for collecting the modulated object beams Ms. The collecting lens 37 has a focal length f₃₇. According to a number of embodiments, the optical system 100 is positioned from the object 10 by a distance substantially equal to the focal length f₃₇ of the collecting lens 37. Accordingly, the modulated object beams Ms are individually collimated by the collecting lens 37 while maintaining the divergence angle ω as the beams Ms travel through the center of the lens 37.

The optical system 100 may also include a focusing lens 39 positioned downstream from the beam combiner or combining element 38 and having a focal length f₃₉. In a number of embodiments, the focusing lens 39 is positioned from the collecting lens 37 by a distance substantially equal to focal length f₃₉. In other embodiments, an output element 111, such as a detector element, may be positioned downstream from the focusing lens 39 by a distance substantially equal to focal length f₃₉.

In still other embodiments, the DOE 47 for splitting the frequency-shifted reference beam R is positioned upstream from the focusing lens 39 by a distance substantially equal to focal length f₃₉. For example, as shown in FIG. 11, the sum of a distance l₁ from DOE 47 to the combining element 38 and a distance l₂ from the combining element 38 to the focusing lens 39 is substantially equal to focal length f₃₉.

Referring to FIG. 12, the optical system 100 may also include an aperture 112 positioned adjacent to the collecting lens 37. The aperture 112 has a diameter d_(AO). In addition, the frequency-shifted reference beams Rs each have a diameter d_(R). According to a number of embodiments, the diameter d_(AO) of the aperture 112 is substantially equal to the diameter d_(R) of the frequency-shifted reference beams Rs. As a result, a diameter d_(M) of the modulated object beams Ms is substantially equal to the diameter d_(R) of the frequency-shifted reference beams Rs.

In other embodiments, the optical system 100 may include a second aperture 114 positioned at an upstream side of DOE 47. The reference-path aperture 114 has a diameter d_(AR). In a number of embodiments, the diameter d_(AR) of the reference-path aperture 114 is substantially equal to the diameter d_(AO) of the object-path aperture 112.

As mentioned above, in a number of embodiments the polarization of the modulated object beams Ms and the polarization of the frequency-shifted reference beams Rs are the same. As shown in FIG. 12, the polarizations are indicated as S-polarization with the dots D.

In addition to collecting the modulated object beams Ms, the collecting lens 37 may also collimate the modulated object beams Ms. The collimated modulated object beams are indicated by Ms′ in FIG. 12. Similarly, the plurality of frequency-shifted reference beams Rs may be collimated by the telescope 110 lens prior to being combined into the beam pairs Ps.

Furthermore, the modulated object beams Ms′ diverge from an optical axis A of the collecting lens 37 at an angle μ. According to a number of embodiments, the divergence angle μ of the modulated object beams Ms′ is substantially equal to the divergence angle ρ of the frequency-shifted reference beams Rs from DOE 47. Also as shown in FIG. 12, the focusing lens 39 may render the plurality of beam pairs Ps substantially parallel with each other, which parallel beam pairs are indicated by Ps′.

With additional reference to FIG. 13, the focusing lens 39 may be positioned a focal length f₃₉ away the output element 111 so that lens 39 focuses each of the parallel beam pairs Ps′ onto the element. As mentioned above, the output element 111 may be an array including a plurality of elements 115, such as photodetectors or optical fibers. Accordingly, the focusing lens 39 focuses each of the beam pairs Ps′ onto a respect one of the elements 115. In embodiments where the elements 115 are optical fibers, a plurality of photodetectors may be provided downstream from the optical fibers. In either embodiment, the output element 111 converts the optical signals of the plurality of beam pairs Ps into the frequency-modulated signals Fs (either analog or digital signals) mentioned above.

The MBLDV 15 of the invention may also be implemented in a scanning multi-beam system 116 as shown in FIG. 14. According to scanning embodiments, the system 116 may include a mirror 118 that is rotatable about an axis A under actuation by a motor 120. The plurality of object beams Os transmitted by the MBLDV 15 may then be reflected off of the mirror 118 simultaneously and onto an object 10 under inspection, as indicated by Os′. The modulated object beams Ms may then be collected by the MBLDV 15. The mirror 118 may then be rotated so that the reflected object beams Os′ are incident at a different location of the object 10. Accordingly, over time a plurality of points t₁, t₂, t₃, t₄, . . . are analyzed by each of the object beams Os′.

One of the advantages of the scanning MBLDV 116 is that the mirror 118 only needs to rotated about a single axis A. Although a two-axis rotatable mirror may be utilized, the single-axis mirror 118 is able to scan a surface of the object 10. More specifically, the MBLDV 15 provides a matrix of a plurality of object beams Os, e.g., an X matrix. The entire matrix may then be scanned in one axis, (e.g., a Y matrix) to provide an X-Y matrix of data. Accordingly, over a relatively short period of time, an entire surface of the object 10 may be scanned by the matrix of object beams and analyzed.

With reference to FIG. 15, according to a number of embodiments, an optical subsystem 71 may include an objective lens assembly 72 having a focus and/or zoom capability and configured to focus the plurality of object beams onto a surface 73 of the target or object 10 and to collect scattered or reflected, modulated beams from the surface 73. Optical subsystem 71 is a particular embodiment of optical subsystem 11 shown in FIG. 2. Optical subsystem 71 may include a laser 18 as a radiation source. An output beam L of the laser 18 may pass through a first half-waveplate (HWP) 29 configured to rotate the polarization of the output beam L and provide variable control of the irradiance of beams downstream thereof.

The output beam L may then be split into an object beam O and a reference beam R at a first polarizing beam splitter (PBS) 30. As shown in the example in FIG. 15, the S-polarized portion of the output beam L is reflected by the PBS 30 and used as the reference beam R, and the P-polarized portion of the output beam L is transmitted by the PBS 30 and used as the object beam O. The object beam O is reflected by a first mirror 74 to provide a first reflected object beam that is applied to a first acousto-optic modulator (AOM) 42 operating at a first frequency f₁ that produces a frequency shift on the reflected object beam to provide a frequency shifted object beam that is reflected from a second mirror 75 and applied to an object beam telescope comprising a lens 32 and a lens 33. The reference beam R is applied to a second acousto-optic modulator (AOM) 43 operating at a second frequency f₂ that produces a frequency shift on the reference beam to provide a frequency shifted reference beam that is reflected from a third mirror 76 and applied to a reference beam telescope comprising a lens 45 and a lens 46.

The output of the object telescope is applied to a first diffractive optical element (DOE) 34 which splits the reflected and shifted object beam into a plurality of object beams Os. Similarly, the output of the reference telescope is applied to a second diffractive optical element (DOE) 47 which splits the reference beam into a plurality of reference beams Rs. Returning to the object path, the plurality of object beams Os may then be transmitted through a second PBS 35, through the focusing lens assembly 72, through a quarter-waveplate (QWP) 36, and then transmitted to the object 10 under inspection by reflection from scanning mirror 118. The plurality of transmitted object beams Ts irradiate substantially and simultaneously a corresponding plurality of points on the object 10 based on the characteristics of the first DOE 34, the characteristics of the focusing lens assembly 72, and the angle of the scanning mirror 118.

Focusing lens assembly 72 may include an f-theta (f-θ) lens satisfying the formula y′=f tan(θ) to yield a distortion-free image. More generally, assembly 72 may comprise transmission optics having a zoom and focus capability where assembly 72 is configured to focus the beams on the object and to select and/or change the spacing between the beams. Assembly 72 may be constructed using a variety of optical components including one or more lenses, filters, or spherical mirrors.

The plurality of object beams Os arriving at the focusing lens assembly 72 from the second PBS 35 are typically collimated and follow the DOE 34 angle. The focusing lens assembly 72 then focuses each and every one of the plurality of object beams Os on the surface 73 of the object 10 and may refine the angle of the object beams Os prior to striking the QWP 36. Vibrations of the object 10 frequency modulate each of the transmitted object beams T substantially simultaneously. A portion of these modulated object beams, which are indicated by Ms, is scattered or reflected back to the optical subsystem 71. Modulated light scattered by the targetted object and collected by the focusing lens assembly 72 follows a reversible path so that beams arriving at the second PBS 35 may be collimated by the focusing lens assembly 72 and then follow a return path of the same angles defined by the plurality of object beams Os. Focusing lens assembly 72 has a focal length f₇₂.

The collimated and focused light passing through lens assembly 72 is applied to the second PBS 35 and reflected as a plurality of beams Ns that are directed to pass through an aperture 112 and then applied to a beam combiner 38, or other suitable combining element. As described in reference to FIG. 12, the aperture 112 has a diameter d_(AO) that is substantially equal to the diameter d_(N) of the reflected and modulated object beams Ns. Beams Ns are symmetrically passed through aperture 112 so that extraneous, or off-angle, light beams are blocked, thereby improving the detection of characteristics in the plurality of beams Ns. The aperture 112 is located at a distance from the lens assembly 72 that is substantially equal to the distance between the DOE 34 and the lens assembly 72. In this manner, a first pair, comprising aperture 112 and DOE 34, and a second pair, comprising aperture 112 and lens assembly 72, form conjugate points. In one embodiment, the beam combiner 38 combines each of the plurality of beams Ns and the plurality of beams Rs in a one-to-one manner to form a plurality of beam pairs Ps that are applied to a collimating lens 39 positioned downstream from the beam combiner 38 and having a focal length f₃₉. The collimating lens 39 may be positioned from the focusing lens assembly 72 by a distance substantially equal to focal length f₃₉. Collimating lens 39 receives the plurality of beam pairs Ps and produces parallel beam pairs that may be focused on a detector array 12. Alternatively, collimating lens 39 may parallelize and focus the beam pairs Ps on an optical conduit, such as a plurality of optical fibers, that conduct light from the beam pairs Ps to a detector array 12.

For the purposes of the following claims, the phenomenon of the transmitted object beams Os being reflected, scattered, and backscattered by the object 10, thereby resulting in the modulated object beams Ms, will be simply indicated by the word ‘reflect’ and its forms, such as ‘reflected’.

Those skilled in the art will understand that the preceding exemplary embodiments of the present invention provide the foundation for numerous alternatives and modifications thereto. For example, although the preceding description set for the principles of the invention in terms of a coherent light source such as a laser, other types of coherent radiation may be utilized, such as microwaves, millimeter waves, and so on. These and other modifications are also within the scope of the present invention. Accordingly, the present invention is not limited to that precisely as shown and described above but by the scope of the appended claims, which are incorporated into this section by reference. 

1. A multi-beam heterodyne vibrometer for analyzing vibration of an object, the vibrometer comprising: an optical system for: generating a plurality of object beams and a plurality of reference beams, one of the plurality of beams having a frequency that is shifted from a frequency of the other plurality of beams; focusing each of the plurality of object beams on the object; transmitting the plurality of focused object beams to the object, a portion of each of the plurality of focused object beams being reflected off of a surface of the object as a modulated object beam; and collecting the modulated object beams; and a combining element for combining each of the modulated object beams with a respective one of the reference beams into a plurality of beam pairs.
 2. The vibrometer of claim 1 wherein the frequency shift is introduced on the one of the plurality of beams prior generating the plurality of object beams and the plurality of reference beams.
 3. The vibrometer of claim 1 wherein the plurality of object beams is frequency shifted.
 4. The vibrometer of claim 1 wherein the plurality of reference beams is frequency shifted.
 5. The vibrometer of claim 1 wherein the plurality of modulated object beams and the plurality of reference beams have the same polarization.
 6. The vibrometer of claim 1 wherein the optical system includes a lens configured to focus the plurality of object beams onto the surface of the object and for collecting the focused modulated object beams.
 7. The vibrometer of claim 6 wherein the lens has a focal length and is positioned from the surface of the object by a distance substantially equal to the focal length.
 8. The vibrometer of claim 6 wherein the lens satisfies the formula y′=f tan(θ) to yield a distortion-free image.
 9. The vibrometer of claim 6 wherein each of the plurality of modulated object beams has a first diameter and the aperture has a second diameter substantially equal to the first diameter.
 10. The vibrometer of claim 1, wherein the optical system includes a first diffractive optical element for splitting an object beam into the plurality of object beams, and wherein the optical system includes an aperture disposed at a distance from the lens that is substantially equal to the distance between the first diffractive optical element and the lens.
 11. The vibrometer of claim 1 wherein the optical system includes a second diffractive optical element for splitting a reference beam into the plurality of reference beams.
 12. The vibrometer of claim 11 wherein the first and second diffractive optical elements are configured to respectively split the plurality of object beams and the plurality of reference beams such that the plurality of object beams and the plurality of reference beams diverge from the respective diffractive optical elements at substantially the same angle.
 13. The vibrometer of claim 1 wherein the optical system further includes: a laser for providing an output beam; and an output beam splitter for splitting the output beam into the object beam and a reference beam, at least one of the beams being frequency shifted prior to being split into the plurality of frequency-shifted beams.
 14. The vibrometer of claim 1 further comprising a mirror for reflecting the transmitted object beams onto the object and a motor for rotating the mirror so that the transmitted object beams scan the object.
 15. A method for analyzing vibration of an object, the method comprising: transmitting a plurality of object beams to the object; focusing each of the plurality of object beams on the object, a portion of the object beams being reflected by the object as modulated object beams; collecting the modulated object beams; and combining the modulated object beams with a reference beam into a plurality of combined beams, wherein one of the combined beams has a frequency that is shifted from a frequency of the other of the combined beams.
 16. The method of claim 15, wherein the operation of focusing each of the plurality of object beams on the object includes the use of a lens satisfying the formula y′=f tan(θ) to yield a distortion-free image.
 17. The method of claim 15, further comprising: analyzing a plurality of combined beams to determine a vibration pattern of the object.
 18. A multi-beam heterodyne vibrometer for analyzing vibration of an object, the vibrometer comprising: an optical system, comprising: a generating means for generating a plurality of object beams and a plurality of reference beams, one of the plurality of beams having a frequency that is shifted from a frequency of the other plurality of beams; a focusing means for focusing each of the plurality of object beams on the object; a transmitting means for transmitting the plurality of focused object beams to the object, a portion of each of the plurality of focused object beams being reflected off of a surface of the object as a modulated object beam; and a collecting means for collecting the modulated object beams; and a combining element for combining each of the modulated object beams with a respective one of the reference beams into a plurality of beam pairs.
 19. The vibrometer of claim 18 wherein the focusing means includes a lens configured to focus the plurality of object beams onto the surface of the object and for collecting the focused modulated object beams, and wherein the lens has a focal length and is positioned from the surface of the object by a distance substantially equal to the focal length.
 20. The vibrometer of claim 19 wherein the lens satisfies the formula y′=f tan(θ) to yield a distortion-free image. 